Tests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections
A 1934 NACA technical report from the NASA Technical Reports Server, testing three tapered wing sections (based on the NACA 2200, NACA-M6 and Clark Y airfoils) for aeronautical engineers and researchers. Its pictures are dense engineering graphs of lift, drag, moment and centre-of-pressure curves against angle of attack, plus a wing root section outline with dimensioned stations, offering a designer little beyond technical line charts and thin airfoil profiles.
